Design objective of high Mach number performance manned flight vehicles is concerned with flight operations such that minimum longitudinal trim drag is achieved; utilization of longitudinal statically unstable vehicles as means of obtaining objective; taking delta wing canard controlled aircraft as example, control concept presented is based on 3 systems of compensating for static instability, mechanical stability augmentation system, autopilot and fuel transfer system; each system is capable of permitting adequate control of aircraft.
Approach to control of statically unstable manned flight vehicles
AGARD -- Report
1961
25 pages
Report
English
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